Attitude control based on inverse system for a spacecraft with zero-momentum wheels

被引：0
|
作者：
Wang, Qing-Chao [1 ]
Hu, Li-Kun [1 ]
机构：
[1] School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
来源：
Dianji yu Kongzhi Xuebao/Electric Machines and Control | 2008年 / 12卷 / 02期
关键词：
Attitude response - Internal model control - Inverse system - Wheel dynamics;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：184 / 189
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